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亚音速飞机压力分布测量 被引量:6

IN FLIGHT MEASUREMENT OF STATIC PRESSURE ON A SUBSONIC TRANSPORT AIRCRAFT
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摘要 简要地介绍了亚音速飞机压力分布测量的飞行试验技术,并给出了部分试验结果。对用测压带法进行机翼压力分布测量及滑流对压力分布的影响等问题进行了讨论。 Technique of in flight measurement of pressure distribution on a subsonic transport aircraft is introduced. Some flight test results are presented. Questions about the measurement of pressure distribution on the wing by using thin pressure belts and the effect of slip flow on pressure distribution are discussed.
作者 原正庭
出处 《航空学报》 EI CAS CSCD 北大核心 1998年第4期486-488,共3页 Acta Aeronautica et Astronautica Sinica
关键词 飞行载荷 压力分布 测压带 亚音速 flight loads, pressure distribution, pressure belts
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  • 1唐宁,白雪.基于应变法飞行实测载荷的机翼压心计算方法[J].现代机械,2020,0(1):46-50. 被引量:4
  • 2宫海波,任晓斌,张振华.机载分布式应变参数采集系统设计[J].中国测试,2021,47(S01):165-168. 被引量:2
  • 3恽起麟.风洞实验数据的误差及其计算方法[J].气动实验与测量控制,1993,7(4):67-77. 被引量:4
  • 4Keener E R,Jordan C H.Wing pressure distribution over the liftrange of the convair XF-92A delta-wing airplane at subsonic and tran-sonic speeds.NACA RM H55G07,November 1955.
  • 5Pyle J S.Flight-measured wing surface pressures and loads for the X-15 airplane at mach numbers from 1.2 to 6.0.NASA TN D-2602,January 1965.
  • 6Montoya L C,Banner R D.F-8 supercritical wing flight pressure,boundary-layer,and wake measurements and comparisons with thewind tunnel data.NASA TM X-3544,June 1977.
  • 7Moes T R,Meyer,Jr R R.In-flight Investigation of shuttle tile pres-sure orifice installations.NASA TM-4219,September 1990.
  • 8Powers S G,Webb L D.Flight wing surface pressure and boudary-layer data report from the F-111 smooth variable-camber supercriti-cal mission adaptive wing.NASA TM-4789,June 1997.
  • 9Landers S F,Saltzman J A.F-16XL wing pressure distributions andshock fence results from Mach 1.4 to Mach 2.0.NASA/TM-97-206219,1997.
  • 10Davis M,Saltzman J.In-flight wing pressure distributions for theNASA F/A-18A high alpha research vehicle.NASA/TP-2000-209018,2000.

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